ENH: interFoam: Merged dynamic mesh functionality of interDyMFoam into interFoam

and replaced interDyMFoam with a script which reports this change.

The interDyMFoam tutorials have been moved into the interFoam directory.

This change is one of a set of developments to merge dynamic mesh functionality
into the standard solvers to improve consistency, usability, flexibility and
maintainability of these solvers.

Henry G. Weller
CFD Direct Ltd.

interMixingFoam, multiphaseInterFoam: Updated for changes to interFoam
This commit is contained in:
Henry Weller
2017-11-30 23:56:42 +00:00
committed by Andrew Heather
parent e50af751a4
commit ede4759b80
266 changed files with 1896 additions and 363 deletions

View File

@ -8,6 +8,7 @@ EXE_INC = \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \ -I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/transportModels/immiscibleIncompressibleTwoPhaseMixture/lnInclude \ -I$(LIB_SRC)/transportModels/immiscibleIncompressibleTwoPhaseMixture/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \ -I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \ -I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude -I$(LIB_SRC)/sampling/lnInclude
@ -16,6 +17,7 @@ EXE_LIBS = \
-lturbulenceModels \ -lturbulenceModels \
-lincompressibleTurbulenceModels \ -lincompressibleTurbulenceModels \
-lfiniteVolume \ -lfiniteVolume \
-ldynamicFvMesh \
-lfvOptions \ -lfvOptions \
-lmeshTools \ -lmeshTools \
-lsampling \ -lsampling \

View File

@ -3,7 +3,7 @@ CorrectPhi
U, U,
phi, phi,
p_rgh, p_rgh,
dimensionedScalar("rAUf", dimTime/rho.dimensions(), 1), surfaceScalarField("rAUf", fvc::interpolate(rAU())),
geometricZeroField(), geometricZeroField(),
pimple pimple
); );

View File

@ -0,0 +1,34 @@
tmp<volScalarField> rAU;
if (correctPhi)
{
rAU = new volScalarField
(
IOobject
(
"rAU",
runTime.timeName(),
mesh,
IOobject::READ_IF_PRESENT,
IOobject::AUTO_WRITE
),
mesh,
dimensionedScalar("rAU", dimTime/dimDensity, 1)
);
#include "correctPhi.H"
}
else
{
CorrectPhi
(
U,
phi,
p_rgh,
dimensionedScalar("rAUf", dimTime/rho.dimensions(), 1),
geometricZeroField(),
pimple
);
#include "continuityErrs.H"
}

View File

@ -1,3 +0,0 @@
interDyMFoam.C
EXE = $(FOAM_APPBIN)/interDyMFoam

View File

@ -1,29 +0,0 @@
EXE_INC = \
-I. \
-I.. \
-I../../VoF \
-I$(LIB_SRC)/transportModels/twoPhaseMixture/lnInclude \
-I$(LIB_SRC)/transportModels \
-I$(LIB_SRC)/transportModels/incompressible/lnInclude \
-I$(LIB_SRC)/transportModels/interfaceProperties/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/transportModels/immiscibleIncompressibleTwoPhaseMixture/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/dynamicMesh/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude
EXE_LIBS = \
-limmiscibleIncompressibleTwoPhaseMixture \
-lturbulenceModels \
-lincompressibleTurbulenceModels \
-lfiniteVolume \
-ldynamicMesh \
-ldynamicFvMesh \
-ltopoChangerFvMesh \
-lmeshTools \
-lfvOptions \
-lsampling \
-lwaveModels

View File

@ -1,11 +0,0 @@
CorrectPhi
(
U,
phi,
p_rgh,
surfaceScalarField("rAUf", fvc::interpolate(rAU())),
geometricZeroField(),
pimple
);
#include "continuityErrs.H"

View File

@ -1,192 +0,0 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
OpenFOAM is free software: you can redistribute it and/or modify it
under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
for more details.
You should have received a copy of the GNU General Public License
along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
Application
interDyMFoam
Group
grpMultiphaseSolvers grpMovingMeshSolvers
Description
Solver for 2 incompressible, isothermal immiscible fluids using a VOF
(volume of fluid) phase-fraction based interface capturing approach,
with optional mesh motion and mesh topology changes including adaptive
re-meshing.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "CMULES.H"
#include "EulerDdtScheme.H"
#include "localEulerDdtScheme.H"
#include "CrankNicolsonDdtScheme.H"
#include "subCycle.H"
#include "immiscibleIncompressibleTwoPhaseMixture.H"
#include "turbulentTransportModel.H"
#include "pimpleControl.H"
#include "fvOptions.H"
#include "CorrectPhi.H"
#include "fvcSmooth.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
#include "postProcess.H"
#include "setRootCase.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "initContinuityErrs.H"
#include "createDyMControls.H"
#include "createFields.H"
#include "createAlphaFluxes.H"
tmp<volScalarField> rAU;
if (correctPhi)
(
rAU = new volScalarField
(
IOobject
(
"rAU",
runTime.timeName(),
mesh,
IOobject::READ_IF_PRESENT,
IOobject::AUTO_WRITE
),
mesh,
dimensionedScalar("rAU", dimTime/dimDensity, 1)
)
);
#include "correctPhi.H"
#include "createUfIfPresent.H"
turbulence->validate();
if (!LTS)
{
#include "CourantNo.H"
#include "setInitialDeltaT.H"
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (runTime.run())
{
#include "readDyMControls.H"
if (LTS)
{
#include "setRDeltaT.H"
}
else
{
#include "CourantNo.H"
#include "alphaCourantNo.H"
#include "setDeltaT.H"
}
runTime++;
Info<< "Time = " << runTime.timeName() << nl << endl;
// --- Pressure-velocity PIMPLE corrector loop
while (pimple.loop())
{
if (pimple.firstIter() || moveMeshOuterCorrectors)
{
mesh.update();
if (mesh.changing())
{
// Do not apply previous time-step mesh compression flux
// if the mesh topology changed
if (mesh.topoChanging())
{
talphaPhi1Corr0.clear();
}
gh = (g & mesh.C()) - ghRef;
ghf = (g & mesh.Cf()) - ghRef;
MRF.update();
}
if ((mesh.changing() && correctPhi) || mesh.topoChanging())
{
// Calculate absolute flux from the mapped surface velocity
// Note: temporary fix until mapped Uf is assessed
Uf = fvc::interpolate(U);
phi = mesh.Sf() & Uf;
#include "correctPhi.H"
// Make the flux relative to the mesh motion
fvc::makeRelative(phi, U);
mixture.correct();
}
if (mesh.changing() && checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
}
#include "alphaControls.H"
#include "alphaEqnSubCycle.H"
mixture.correct();
#include "UEqn.H"
// --- Pressure corrector loop
while (pimple.correct())
{
#include "pEqn.H"
}
if (pimple.turbCorr())
{
turbulence->correct();
}
}
runTime.write();
runTime.printExecutionTime(Info);
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //

View File

@ -1,81 +0,0 @@
{
rAU = 1.0/UEqn.A();
surfaceScalarField rAUf("rAUf", fvc::interpolate(rAU()));
volVectorField HbyA(constrainHbyA(rAU()*UEqn.H(), U, p_rgh));
surfaceScalarField phiHbyA
(
"phiHbyA",
fvc::flux(HbyA)
+ fvc::interpolate(rho*rAU())*fvc::ddtCorr(U, phi, Uf)
);
MRF.makeRelative(phiHbyA);
if (p_rgh.needReference())
{
fvc::makeRelative(phiHbyA, U);
adjustPhi(phiHbyA, U, p_rgh);
fvc::makeAbsolute(phiHbyA, U);
}
surfaceScalarField phig
(
(
mixture.surfaceTensionForce()
- ghf*fvc::snGrad(rho)
)*rAUf*mesh.magSf()
);
phiHbyA += phig;
// Update the pressure BCs to ensure flux consistency
constrainPressure(p_rgh, U, phiHbyA, rAUf, MRF);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix p_rghEqn
(
fvm::laplacian(rAUf, p_rgh) == fvc::div(phiHbyA)
);
p_rghEqn.setReference(pRefCell, getRefCellValue(p_rgh, pRefCell));
p_rghEqn.solve(mesh.solver(p_rgh.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA - p_rghEqn.flux();
p_rgh.relax();
U = HbyA + rAU()*fvc::reconstruct((phig - p_rghEqn.flux())/rAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
}
}
#include "continuityErrs.H"
// Correct Uf if the mesh is moving
fvc::correctUf(Uf, U, phi);
// Make the fluxes relative to the mesh motion
fvc::makeRelative(phi, U);
p == p_rgh + rho*gh;
if (p_rgh.needReference())
{
p += dimensionedScalar
(
"p",
p.dimensions(),
pRefValue - getRefCellValue(p, pRefCell)
);
p_rgh = p - rho*gh;
}
if (!correctPhi)
{
rAU.clear();
}
}

View File

@ -29,18 +29,14 @@ Group
Description Description
Solver for 2 incompressible, isothermal immiscible fluids using a VOF Solver for 2 incompressible, isothermal immiscible fluids using a VOF
(volume of fluid) phase-fraction based interface capturing approach. (volume of fluid) phase-fraction based interface capturing approach,
with optional mesh motion and mesh topology changes including adaptive
The momentum and other fluid properties are of the "mixture" and a single re-meshing.
momentum equation is solved.
Turbulence modelling is generic, i.e. laminar, RAS or LES may be selected.
For a two-fluid approach see twoPhaseEulerFoam.
\*---------------------------------------------------------------------------*/ \*---------------------------------------------------------------------------*/
#include "fvCFD.H" #include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "CMULES.H" #include "CMULES.H"
#include "EulerDdtScheme.H" #include "EulerDdtScheme.H"
#include "localEulerDdtScheme.H" #include "localEulerDdtScheme.H"
@ -61,30 +57,28 @@ int main(int argc, char *argv[])
#include "setRootCase.H" #include "setRootCase.H"
#include "createTime.H" #include "createTime.H"
#include "createMesh.H" #include "createDynamicFvMesh.H"
#include "createControl.H"
#include "createTimeControls.H"
#include "initContinuityErrs.H" #include "initContinuityErrs.H"
#include "createDyMControls.H"
#include "createFields.H" #include "createFields.H"
#include "createAlphaFluxes.H" #include "createAlphaFluxes.H"
#include "correctPhi.H" #include "initCorrectPhi.H"
#include "createUfIfPresent.H"
turbulence->validate(); turbulence->validate();
if (!LTS) if (!LTS)
{ {
#include "readTimeControls.H"
#include "CourantNo.H" #include "CourantNo.H"
#include "setInitialDeltaT.H" #include "setInitialDeltaT.H"
} }
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl; Info<< "\nStarting time loop\n" << endl;
while (runTime.run()) while (runTime.run())
{ {
#include "readTimeControls.H" #include "readDyMControls.H"
if (LTS) if (LTS)
{ {
@ -104,6 +98,45 @@ int main(int argc, char *argv[])
// --- Pressure-velocity PIMPLE corrector loop // --- Pressure-velocity PIMPLE corrector loop
while (pimple.loop()) while (pimple.loop())
{ {
if (pimple.firstIter() || moveMeshOuterCorrectors)
{
mesh.update();
if (mesh.changing())
{
// Do not apply previous time-step mesh compression flux
// if the mesh topology changed
if (mesh.topoChanging())
{
talphaPhi1Corr0.clear();
}
gh = (g & mesh.C()) - ghRef;
ghf = (g & mesh.Cf()) - ghRef;
MRF.update();
if (correctPhi)
{
// Calculate absolute flux
// from the mapped surface velocity
phi = mesh.Sf() & Uf();
#include "correctPhi.H"
// Make the flux relative to the mesh motion
fvc::makeRelative(phi, U);
mixture.correct();
}
if (checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
}
}
#include "alphaControls.H" #include "alphaControls.H"
#include "alphaEqnSubCycle.H" #include "alphaEqnSubCycle.H"

View File

@ -11,6 +11,7 @@ EXE_INC = \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \ -I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \ -I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \ -I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/transportModels \ -I$(LIB_SRC)/transportModels \
-I$(LIB_SRC)/meshTools/lnInclude \ -I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude -I$(LIB_SRC)/sampling/lnInclude

View File

@ -53,11 +53,11 @@ int main(int argc, char *argv[])
#include "setRootCase.H" #include "setRootCase.H"
#include "createTime.H" #include "createTime.H"
#include "createMesh.H" #include "createMesh.H"
#include "createControl.H"
#include "createTimeControls.H"
#include "initContinuityErrs.H" #include "initContinuityErrs.H"
#include "createDyMControls.H"
#include "createFields.H" #include "createFields.H"
#include "correctPhi.H" #include "initCorrectPhi.H"
#include "createUfIfPresent.H"
turbulence->validate(); turbulence->validate();
@ -74,7 +74,7 @@ int main(int argc, char *argv[])
while (runTime.run()) while (runTime.run())
{ {
#include "readTimeControls.H" #include "readDyMControls.H"
if (LTS) if (LTS)
{ {

View File

@ -1,17 +1,29 @@
{ {
volScalarField rAU("rAU", 1.0/UEqn.A()); if (correctPhi)
surfaceScalarField rAUf("rAUf", fvc::interpolate(rAU)); {
rAU.ref() = 1.0/UEqn.A();
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p_rgh)); }
else
{
rAU = 1.0/UEqn.A();
}
surfaceScalarField rAUf("rAUf", fvc::interpolate(rAU()));
volVectorField HbyA(constrainHbyA(rAU()*UEqn.H(), U, p_rgh));
surfaceScalarField phiHbyA surfaceScalarField phiHbyA
( (
"phiHbyA", "phiHbyA",
fvc::flux(HbyA) fvc::flux(HbyA)
+ fvc::interpolate(rho*rAU)*fvc::ddtCorr(U, phi) + fvc::interpolate(rho*rAU())*fvc::ddtCorr(U, phi, Uf)
); );
MRF.makeRelative(phiHbyA); MRF.makeRelative(phiHbyA);
adjustPhi(phiHbyA, U, p_rgh);
if (p_rgh.needReference())
{
fvc::makeRelative(phiHbyA, U);
adjustPhi(phiHbyA, U, p_rgh);
fvc::makeAbsolute(phiHbyA, U);
}
surfaceScalarField phig surfaceScalarField phig
( (
@ -43,7 +55,7 @@
p_rgh.relax(); p_rgh.relax();
U = HbyA + rAU*fvc::reconstruct((phig - p_rghEqn.flux())/rAUf); U = HbyA + rAU()*fvc::reconstruct((phig - p_rghEqn.flux())/rAUf);
U.correctBoundaryConditions(); U.correctBoundaryConditions();
fvOptions.correct(U); fvOptions.correct(U);
} }
@ -51,6 +63,12 @@
#include "continuityErrs.H" #include "continuityErrs.H"
// Correct Uf if the mesh is moving
fvc::correctUf(Uf, U, phi);
// Make the fluxes relative to the mesh motion
fvc::makeRelative(phi, U);
p == p_rgh + rho*gh; p == p_rgh + rho*gh;
if (p_rgh.needReference()) if (p_rgh.needReference())
@ -63,4 +81,9 @@
); );
p_rgh = p - rho*gh; p_rgh = p - rho*gh;
} }
if (!correctPhi)
{
rAU.clear();
}
} }

View File

@ -9,6 +9,7 @@ EXE_INC = \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \ -I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \ -I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \ -I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \ -I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude -I$(LIB_SRC)/sampling/lnInclude

View File

@ -1,7 +1,6 @@
EXE_INC = \ EXE_INC = \
-I.. \ -I.. \
-I../../VoF \ -I../../VoF \
-I../../interFoam/interDyMFoam \
-I../../interFoam \ -I../../interFoam \
-I../multiphaseMixture/lnInclude \ -I../multiphaseMixture/lnInclude \
-I$(LIB_SRC)/transportModels \ -I$(LIB_SRC)/transportModels \

View File

@ -51,16 +51,17 @@ int main(int argc, char *argv[])
#include "setRootCase.H" #include "setRootCase.H"
#include "createTime.H" #include "createTime.H"
#include "createMesh.H" #include "createMesh.H"
#include "createControl.H"
#include "initContinuityErrs.H" #include "initContinuityErrs.H"
#include "createDyMControls.H"
#include "createFields.H" #include "createFields.H"
#include "createTimeControls.H" #include "initCorrectPhi.H"
#include "correctPhi.H" #include "createUfIfPresent.H"
#include "CourantNo.H"
#include "setInitialDeltaT.H"
turbulence->validate(); turbulence->validate();
#include "CourantNo.H"
#include "setInitialDeltaT.H"
const surfaceScalarField& rhoPhi(mixture.rhoPhi()); const surfaceScalarField& rhoPhi(mixture.rhoPhi());
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -69,7 +70,7 @@ int main(int argc, char *argv[])
while (runTime.run()) while (runTime.run())
{ {
#include "readTimeControls.H" #include "readDyMControls.H"
#include "CourantNo.H" #include "CourantNo.H"
#include "alphaCourantNo.H" #include "alphaCourantNo.H"
#include "setDeltaT.H" #include "setDeltaT.H"

View File

@ -1,6 +1,6 @@
EXE_INC = \ EXE_INC = \
-I.. \ -I.. \
-I../../interFoam/interDyMFoam \ -I../../interFoam \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \ -I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \ -I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/transportModels \ -I$(LIB_SRC)/transportModels \

38
bin/interDyMFoam Executable file
View File

@ -0,0 +1,38 @@
#!/bin/sh
#------------------------------------------------------------------------------
# ========= |
# \\ / F ield | OpenFOAM: The Open Source CFD Toolbox
# \\ / O peration |
# \\ / A nd | Copyright (C) 2017 OpenFOAM Foundation
# \\/ M anipulation |
#-------------------------------------------------------------------------------
# License
# This file is part of OpenFOAM.
#
# OpenFOAM is free software: you can redistribute it and/or modify it
# under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
#
# OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
# ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
# FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
# for more details.
#
# You should have received a copy of the GNU General Public License
# along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
#
# Script
# supersededByPostProcess
#
# Description
# Script to suggest using the new "postProcess" utility.
#
#------------------------------------------------------------------------------
DyMsolver=${0##*/}
solver=$(echo $DyMsolver | sed 's/DyM//')
echo "The dynamic mesh functionality in $DyMsolver has been merged into $solver"
echo "and the $DyMsolver tutorials moved into the $solver tutorials directory"
#------------------------------------------------------------------------------

View File

@ -15,7 +15,7 @@ FoamFile
} }
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application interDyMFoam; application interFoam;
startFrom startTime; startFrom startTime;

View File

@ -15,7 +15,7 @@ FoamFile
} }
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application interDyMFoam; application interFoam;
startFrom startTime; startFrom startTime;

View File

@ -0,0 +1,72 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Umean 1.668;
mUmean -1.668;
dimensions [0 1 -1 0 0 0 0];
internalField uniform ($mUmean 0 0);
boundaryField
{
//- Set patchGroups for constraint patches
#includeEtc "caseDicts/setConstraintTypes"
inlet
{
type waveVelocity;
origin (0 0 0.244);
direction (-1 0 0);
speed $Umean;
waves
(
Stokes2
{
length 3;
amplitude 0.04;
phase 0;
angle 0;
}
);
scale table ((4 1) (12 0));
}
outlet
{
type outletPhaseMeanVelocity;
alpha alpha.water;
Umean $Umean;
value $internalField;
}
atmosphere
{
type pressureInletOutletVelocity;
tangentialVelocity $internalField;
value uniform (0 0 0);
}
hull
{
type movingWallVelocity;
value uniform (0 0 0);
}
}
// ************************************************************************* //

View File

@ -0,0 +1,53 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alpha;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
//- Set patchGroups for constraint patches
#includeEtc "caseDicts/setConstraintTypes"
inlet
{
type waveAlpha;
}
outlet
{
type variableHeightFlowRate;
lowerBound 0;
upperBound 1;
value $internalField;
}
atmosphere
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
hull
{
type zeroGradient;
}
}
// ************************************************************************* //

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@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.00015;
boundaryField
{
//- Set patchGroups for constraint patches
#includeEtc "caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
atmosphere
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
hull
{
type kqRWallFunction;
value $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,53 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 5e-07;
boundaryField
{
//- Set patchGroups for constraint patches
#includeEtc "caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type zeroGradient;
}
atmosphere
{
type zeroGradient;
}
hull
{
type nutkRoughWallFunction;
Ks uniform 100e-6;
Cs uniform 0.5;
value $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,56 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 -1 0 0 0 0];
internalField uniform 2;
boundaryField
{
//- Set patchGroups for constraint patches
#includeEtc "caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
atmosphere
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
hull
{
type omegaWallFunction;
value $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object p_rgh;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
//- Set patchGroups for constraint patches
#includeEtc "caseDicts/setConstraintTypes"
inlet
{
type fixedFluxPressure;
value $internalField;
}
outlet
{
type zeroGradient;
}
atmosphere
{
type totalPressure;
p0 uniform 0;
}
hull
{
type fixedFluxPressure;
value $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,52 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class pointVectorField;
location "0";
object pointDisplacement;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
//- Set patchGroups for constraint patches
#includeEtc "caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value uniform (0 0 0);
}
outlet
{
type fixedValue;
value uniform (0 0 0);
}
atmosphere
{
type fixedValue;
value uniform (0 0 0);
}
hull
{
type calculated;
}
}
// ************************************************************************* //

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@ -0,0 +1,17 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
# remove surface
rm -f constant/triSurface/DTC-scaled.stl.gz > /dev/null 2>&1
rm -rf constant/extendedFeatureEdgeMesh > /dev/null 2>&1
rm -f constant/triSurface/DTC-scaled.eMesh > /dev/null 2>&1
cleanCase
rm constant/polyMesh/boundary > /dev/null 2>&1
rm -rf 0 > /dev/null 2>&1
rm system/topoSetDict > /dev/null 2>&1
#------------------------------------------------------------------------------

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@ -0,0 +1,37 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# copy DTC hull surface from resources folder
cp $FOAM_TUTORIALS/resources/geometry/DTC-scaled.stl.gz constant/triSurface/
runApplication surfaceFeatureExtract
runApplication blockMesh
for i in 1 2 3 4 5 6
do
runApplication -s $i \
topoSet -dict system/topoSetDict.${i}
runApplication -s $i \
refineMesh -dict system/refineMeshDict -overwrite
done
runApplication snappyHexMesh -overwrite
rm -rf 0
cp -r 0.orig 0
runApplication setWaves -alpha alpha.water
runApplication decomposePar
runParallel renumberMesh -overwrite
runParallel $(getApplication)
runApplication reconstructPar

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@ -0,0 +1,83 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object dynamicMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dynamicFvMesh dynamicMotionSolverFvMesh;
motionSolverLibs ("librigidBodyMeshMotion.so");
motionSolver rigidBodyMotion;
report on;
solver
{
type Newmark;
}
accelerationRelaxation 0.4;
bodies
{
hull
{
type rigidBody;
parent root;
centreOfMass (0 0 0);
mass 412.73;
inertia (40 0 0 921 0 921);
transform (1 0 0 0 1 0 0 0 1) (2.929541 0 0.2);
joint
{
type composite;
joints
(
{
type Pz;
}
{
type Ry;
}
);
}
patches (hull);
innerDistance 0.3;
outerDistance 1;
}
}
restraints
{
translationDamper
{
type linearDamper;
body hull;
coeff 8596;
}
rotationDamper
{
type sphericalAngularDamper;
body hull;
coeff 11586;
}
}
// ************************************************************************* //

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@ -0,0 +1,21 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedVectorField;
location "constant";
object g;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value (0 0 -9.81);
// ************************************************************************* //

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@ -0,0 +1,21 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedScalarField;
location "constant";
object hRef;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
value 0.244;
// ************************************************************************* //

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@ -0,0 +1,36 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
phases (water air);
water
{
transportModel Newtonian;
nu 1.09e-06;
rho 998.8;
}
air
{
transportModel Newtonian;
nu 1.48e-05;
rho 1;
}
sigma 0;
// ************************************************************************* //

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@ -0,0 +1,4 @@
Folder to house tri-surfaces
The Allrun script copies the surface from the $FOAM_TUTORIALS/resources/geometry
folder

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@ -0,0 +1,30 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
RASModel kOmegaSST;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

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@ -0,0 +1,148 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(-20 -10 -10)
(10 -10 -10)
(10 0 -10)
(-20 0 -10)
(-20 -10 -1.112)
(10 -10 -1.112)
(10 0 -1.112)
(-20 0 -1.112)
(-20 -10 0.188)
(10 -10 0.188)
(10 0 0.188)
(-20 0 0.188)
(-20 -10 0.244)
(10 -10 0.244)
(10 0 0.244)
(-20 0 0.244)
(-20 -10 0.3)
(10 -10 0.3)
(10 0 0.3)
(-20 0 0.3)
(-20 -10 1.6)
(10 -10 1.6)
(10 0 1.6)
(-20 0 1.6)
(-20 -10 4)
(10 -10 4)
(10 0 4)
(-20 0 4)
);
blocks
(
hex (0 1 2 3 4 5 6 7) (30 10 30) simpleGrading (1 1 0.05)
hex (4 5 6 7 8 9 10 11) (30 10 40) simpleGrading (1 1 1)
hex (8 9 10 11 12 13 14 15) (30 10 4) simpleGrading (1 1 1)
hex (12 13 14 15 16 17 18 19) (30 10 4) simpleGrading (1 1 1)
hex (16 17 18 19 20 21 22 23) (30 10 40) simpleGrading (1 1 1)
hex (20 21 22 23 24 25 26 27) (30 10 10) simpleGrading (1 1 20)
);
edges
(
);
boundary
(
atmosphere
{
type patch;
faces
(
(24 25 26 27)
);
}
inlet
{
type patch;
faces
(
(1 2 6 5)
(5 6 10 9)
(9 10 14 13)
(13 14 18 17)
(17 18 22 21)
(21 22 26 25)
);
}
outlet
{
type patch;
faces
(
(0 4 7 3)
(4 8 11 7)
(8 12 15 11)
(12 16 19 15)
(16 20 23 19)
(20 24 27 23)
);
}
bottom
{
type symmetryPlane;
faces
(
(0 3 2 1)
);
}
side
{
type symmetryPlane;
faces
(
(0 1 5 4)
(4 5 9 8)
(8 9 13 12)
(12 13 17 16)
(16 17 21 20)
(20 21 25 24)
);
}
midPlane
{
type symmetryPlane;
faces
(
(3 7 6 2)
(7 11 10 6)
(11 15 14 10)
(15 19 18 14)
(19 23 22 18)
(23 27 26 22)
);
}
);
mergePatchPairs
(
);
// ************************************************************************* //

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@ -0,0 +1,87 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application interFoam;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 20;
deltaT 0.0001;
writeControl adjustableRunTime;
writeInterval 5;
purgeWrite 0;
writeFormat binary;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxCo 20;
maxAlphaCo 15;
maxDeltaT 0.01;
libs ("libwaves.so");
functions
{
surfaces
{
type surfaces;
libs ("libsampling.so");
writeControl adjustableRunTime;
writeInterval 0.01;
timeStart 10;
surfaceFormat vtk;
fields (p_rgh U);
interpolationScheme cellPoint;
surfaces
(
interface
{
type isoSurface;
isoField alpha.water;
isoValue 0.5;
interpolate true;
}
);
}
}
// ************************************************************************* //

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@ -0,0 +1,23 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
numberOfSubdomains 8;
method scotch;
// ************************************************************************* //

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@ -0,0 +1,60 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
limitedGrad cellLimited Gauss linear 1;
}
divSchemes
{
div(rhoPhi,U) Gauss linearUpwind grad(U);
div(phi,alpha) Gauss vanLeer;
div(phirb,alpha) Gauss linear;
div(phi,k) Gauss linearUpwind limitedGrad;
div(phi,omega) Gauss linearUpwind limitedGrad;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
wallDist
{
method meshWave;
}
// ************************************************************************* //

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@ -0,0 +1,104 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"alpha.water.*"
{
nAlphaCorr 3;
nAlphaSubCycles 1;
cAlpha 1;
icAlpha 0;
MULESCorr yes;
nLimiterIter 15;
alphaApplyPrevCorr yes;
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-10;
relTol 0;
minIter 1;
}
"pcorr.*"
{
solver GAMG;
smoother DIC;
tolerance 1e-3;
relTol 0;
};
p_rgh
{
solver GAMG;
smoother DIC;
tolerance 5e-8;
relTol 0;
};
p_rghFinal
{
$p_rgh;
relTol 0;
}
"(U|k|omega).*"
{
solver smoothSolver;
smoother symGaussSeidel;
nSweeps 1;
tolerance 1e-7;
relTol 0;
minIter 1;
};
}
PIMPLE
{
momentumPredictor no;
nOuterCorrectors 3;
nCorrectors 1;
nNonOrthogonalCorrectors 0;
correctPhi yes;
moveMeshOuterCorrectors yes;
turbOnFinalIterOnly yes;
}
relaxationFactors
{
equations
{
".*" 1;
}
}
cache
{
grad(U);
}
// ************************************************************************* //

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@ -0,0 +1,86 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object meshQualityDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
//- Maximum non-orthogonality allowed. Set to 180 to disable.
maxNonOrtho 70;
//- Max skewness allowed. Set to <0 to disable.
maxBoundarySkewness 20;
maxInternalSkewness 4;
//- Max concaveness allowed. Is angle (in degrees) below which concavity
// is allowed. 0 is straight face, <0 would be convex face.
// Set to 180 to disable.
maxConcave 80;
//- Minimum pyramid volume. Is absolute volume of cell pyramid.
// Set to a sensible fraction of the smallest cell volume expected.
// Set to very negative number (e.g. -1E30) to disable.
minVol 1e-13;
//- Minimum quality of the tet formed by the face-centre
// and variable base point minimum decomposition triangles and
// the cell centre. Set to very negative number (e.g. -1E30) to
// disable.
// <0 = inside out tet,
// 0 = flat tet
// 1 = regular tet
minTetQuality 1e-30;
//- Minimum face area. Set to <0 to disable.
minArea -1;
//- Minimum face twist. Set to <-1 to disable. dot product of face normal
// and face centre triangles normal
minTwist 0.05;
//- Minimum normalised cell determinant
// 1 = hex, <= 0 = folded or flattened illegal cell
minDeterminant 0.001;
//- minFaceWeight (0 -> 0.5)
minFaceWeight 0.05;
//- minVolRatio (0 -> 1)
minVolRatio 0.01;
//must be >0 for Fluent compatibility
minTriangleTwist -1;
//- If >0 : preserve single cells with all points on the surface if the
// resulting volume after snapping (by approximation) is larger than
// minVolCollapseRatio times old volume (i.e. not collapsed to flat cell).
// If <0 : delete always.
//minVolCollapseRatio 0.5;
// Advanced
//- Number of error distribution iterations
nSmoothScale 4;
//- Amount to scale back displacement at error points
errorReduction 0.75;
// Optional : some meshing phases allow usage of relaxed rules.
// See e.g. addLayersControls::nRelaxedIter.
relaxed
{
//- Maximum non-orthogonality allowed. Set to 180 to disable.
maxNonOrtho 75;
}

View File

@ -0,0 +1,43 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object refineMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
set c0;
coordinateSystem global;
globalCoeffs
{
tan1 (1 0 0);
tan2 (0 1 0);
}
patchLocalCoeffs
{
patch outside;
tan1 (1 0 0);
}
directions ( tan1 tan2 );
useHexTopology no;
geometricCut yes;
writeMesh no;
// ************************************************************************* //

View File

@ -0,0 +1,285 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object snappyHexMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Which of the steps to run
castellatedMesh true;
snap true;
addLayers true;
// Geometry. Definition of all surfaces. All surfaces are of class
// searchableSurface.
// Surfaces are used
// - to specify refinement for any mesh cell intersecting it
// - to specify refinement for any mesh cell inside/outside/near
// - to 'snap' the mesh boundary to the surface
geometry
{
hull
{
type triSurfaceMesh;
file "DTC-scaled.stl";
patchInfo
{
type wall;
}
}
};
// Settings for the castellatedMesh generation.
castellatedMeshControls
{
// Refinement parameters
// ~~~~~~~~~~~~~~~~~~~~~
// If local number of cells is >= maxLocalCells on any processor
// switches from from refinement followed by balancing
// (current method) to (weighted) balancing before refinement.
maxLocalCells 100000;
// Overall cell limit (approximately). Refinement will stop immediately
// upon reaching this number so a refinement level might not complete.
// Note that this is the number of cells before removing the part which
// is not 'visible' from the keepPoint. The final number of cells might
// actually be a lot less.
maxGlobalCells 2000000;
// The surface refinement loop might spend lots of iterations refining just a
// few cells. This setting will cause refinement to stop if <= minimumRefine
// are selected for refinement. Note: it will at least do one iteration
// (unless the number of cells to refine is 0)
minRefinementCells 0;
// Number of buffer layers between different levels.
// 1 means normal 2:1 refinement restriction, larger means slower
// refinement.
nCellsBetweenLevels 3;
// Explicit feature edge refinement
// ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
// Specifies a level for any cell intersected by its edges.
// This is a featureEdgeMesh, read from constant/triSurface for now.
features
(
{
file "DTC-scaled.eMesh";
level 0;
}
);
// Surface based refinement
// ~~~~~~~~~~~~~~~~~~~~~~~~
// Specifies two levels for every surface. The first is the minimum level,
// every cell intersecting a surface gets refined up to the minimum level.
// The second level is the maximum level. Cells that 'see' multiple
// intersections where the intersections make an
// angle > resolveFeatureAngle get refined up to the maximum level.
refinementSurfaces
{
hull
{
// Surface-wise min and max refinement level
level (0 0);
}
}
resolveFeatureAngle 45;
// Region-wise refinement
// ~~~~~~~~~~~~~~~~~~~~~~
// Specifies refinement level for cells in relation to a surface. One of
// three modes
// - distance. 'levels' specifies per distance to the surface the
// wanted refinement level. The distances need to be specified in
// descending order.
// - inside. 'levels' is only one entry and only the level is used. All
// cells inside the surface get refined up to the level. The surface
// needs to be closed for this to be possible.
// - outside. Same but cells outside.
refinementRegions
{
}
// Mesh selection
// ~~~~~~~~~~~~~~
// After refinement patches get added for all refinementSurfaces and
// all cells intersecting the surfaces get put into these patches. The
// section reachable from the locationInMesh is kept.
// NOTE: This point should never be on a face, always inside a cell, even
// after refinement.
locationInMesh (-0.7 0 0);
// Whether any faceZones (as specified in the refinementSurfaces)
// are only on the boundary of corresponding cellZones or also allow
// free-standing zone faces. Not used if there are no faceZones.
allowFreeStandingZoneFaces true;
}
// Settings for the snapping.
snapControls
{
//- Number of patch smoothing iterations before finding correspondence
// to surface
nSmoothPatch 3;
//- Relative distance for points to be attracted by surface feature point
// or edge. True distance is this factor times local
// maximum edge length.
// tolerance 4.0;
tolerance 1.0;
//- Number of mesh displacement relaxation iterations.
nSolveIter 100;
//- Maximum number of snapping relaxation iterations. Should stop
// before upon reaching a correct mesh.
nRelaxIter 5;
nFeatureSnapIter 10;
}
// Settings for the layer addition.
addLayersControls
{
// Are the thickness parameters below relative to the undistorted
// size of the refined cell outside layer (true) or absolute sizes (false).
relativeSizes true;
// Per final patch (so not geometry!) the layer information
layers
{
hull
{
nSurfaceLayers 3;
}
}
// Expansion factor for layer mesh
expansionRatio 1.5;
// Wanted thickness of final added cell layer. If multiple layers
// is the thickness of the layer furthest away from the wall.
// Relative to undistorted size of cell outside layer.
// See relativeSizes parameter.
finalLayerThickness 0.7;
// Minimum thickness of cell layer. If for any reason layer
// cannot be above minThickness do not add layer.
// See relativeSizes parameter.
minThickness 0.25;
// If points get not extruded do nGrow layers of connected faces that are
// also not grown. This helps convergence of the layer addition process
// close to features.
// Note: changed(corrected) w.r.t 17x! (didn't do anything in 17x)
nGrow 0;
// Advanced settings
// When not to extrude surface. 0 is flat surface, 90 is when two faces
// are perpendicular
featureAngle 60;
// Maximum number of snapping relaxation iterations. Should stop
// before upon reaching a correct mesh.
nRelaxIter 5;
// Number of smoothing iterations of surface normals
nSmoothSurfaceNormals 1;
// Number of smoothing iterations of interior mesh movement direction
nSmoothNormals 3;
// Smooth layer thickness over surface patches
nSmoothThickness 10;
// Stop layer growth on highly warped cells
maxFaceThicknessRatio 0.5;
// Reduce layer growth where ratio thickness to medial
// distance is large
maxThicknessToMedialRatio 0.3;
// Angle used to pick up medial axis points
// Note: changed(corrected) w.r.t 17x! 90 degrees corresponds to 130 in 17x.
minMedianAxisAngle 90;
// Create buffer region for new layer terminations
nBufferCellsNoExtrude 0;
// Overall max number of layer addition iterations. The mesher will exit
// if it reaches this number of iterations; possibly with an illegal
// mesh.
nLayerIter 50;
// Max number of iterations after which relaxed meshQuality controls
// get used. Up to nRelaxIter it uses the settings in meshQualityControls,
// after nRelaxIter it uses the values in meshQualityControls::relaxed.
nRelaxedIter 20;
}
// Generic mesh quality settings. At any undoable phase these determine
// where to undo.
meshQualityControls
{
#include "meshQualityDict"
}
// Advanced
// Flags for optional output
// 0 : only write final meshes
// 1 : write intermediate meshes
// 2 : write volScalarField with cellLevel for postprocessing
// 4 : write current intersections as .obj files
debug 0;
// Merge tolerance. Is fraction of overall bounding box of initial mesh.
// Note: the write tolerance needs to be higher than this.
mergeTolerance 1E-6;
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object surfaceFeatureExtractDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
DTC-scaled.stl
{
// How to obtain raw features (extractFromFile || extractFromSurface)
extractionMethod extractFromSurface;
extractFromSurfaceCoeffs
{
// Mark edges whose adjacent surface normals are at an angle less
// than includedAngle as features
// - 0 : selects no edges
// - 180: selects all edges
includedAngle 150;
}
subsetFeatures
{
// Keep nonManifold edges (edges with >2 connected faces)
nonManifoldEdges yes;
// Keep open edges (edges with 1 connected face)
openEdges yes;
}
// Write options
// Write features to obj format for postprocessing
writeObj yes;
}
// ************************************************************************* //

View File

@ -0,0 +1,32 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name c0;
type cellSet;
action new;
source boxToCell;
sourceInfo
{
box (-4 -5 -3) (10 0 3);
}
}
);
// ************************************************************************* //

View File

@ -0,0 +1,32 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name c0;
type cellSet;
action new;
source boxToCell;
sourceInfo
{
box (-3 -3 -2.5) (10 0 2);
}
}
);
// ************************************************************************* //

View File

@ -0,0 +1,32 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name c0;
type cellSet;
action new;
source boxToCell;
sourceInfo
{
box (-2 -1.5 -1) (10 0 1.5);
}
}
);
// ************************************************************************* //

View File

@ -0,0 +1,32 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name c0;
type cellSet;
action new;
source boxToCell;
sourceInfo
{
box (-1 -1 -0.6) (10 0 1);
}
}
);
// ************************************************************************* //

View File

@ -0,0 +1,32 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name c0;
type cellSet;
action new;
source boxToCell;
sourceInfo
{
box (-0.5 -0.6 -0.3) (10 0 0.8);
}
}
);
// ************************************************************************* //

View File

@ -0,0 +1,32 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name c0;
type cellSet;
action new;
source boxToCell;
sourceInfo
{
box (-0.25 -0.55 -0.15) (6.25 0 0.65);
}
}
);
// ************************************************************************* //

View File

@ -15,7 +15,7 @@ FoamFile
} }
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application interDyMFoam; application interFoam;
startFrom startTime; startFrom startTime;

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